// FAA AIRWORTHINESS DIRECTIVES
FAA Airworthiness Directives
Search AD numbers, titles, or models across the FAA database.
| No | AD Number | Title | Model | Superseded AD | Superseded By | Actions |
|---|---|---|---|---|---|---|
| 1 | FAA 2002-02-06 | Rear Engine Mount -- Fail-Safe Link | A330-243 | A330-341 | A330-342 | A330-343 | |||
| 2 | FAA 2001-15-18 | Stage Compressor Disks | JT8D-11 | JT8D-15 | JT8D-15A | JT8D-17 | JT8D-17A | JT8D-17AR | JT8D-17R | JT8D-9 | JT8D-9A | |||
| 3 | FAA 2001-02-03 | Raised Forging Boss | 206A | 206B | 206L | 206L-1 | 206L-3 | |||
| 4 | FAA 2000-17-04 | Fuselage Lap Joint | 737-100 Series | 737-200 Series | 737-200C Series | FAA 2003-23-03 | ||
| 5 | FAA 2000-03-22 | Taperlock Bolts in the Diagonal Brace Underwing Fittings | 747-100 Series | 747-100B Series | 747-100B SUD Series | 747-200B Series | 747-200C Series | 747-200F Series | 747SP Series | |||
| 6 | FAA 99-21-04 | Fuselage Belly Fairing Support Structure | A330-301 | A340-211 | A340-212 | A340-311 | A340-312 | |||
| 7 | FAA 99-07-02 | Main Rotor Blade | AS332C | AS332L | AS332L1 | AS332L2 | SA330F | SA330G | SA330J | |||
| 8 | FAA 98-20-13 | Fuselage Skin Panels Corrosion Inspection | A300 B2-1A | A300 B2-1C | A300 B2-203 | A300 B2K-3C | A300 B4-103 | A300 B4-203 | A300 B4-2C | |||
| 9 | FAA 98-09-24 | Elevator Rib Area Damage Inspection | H-36 DIMONA | HK 36 R SUPER DIMONA | |||
| 10 | FAA 97-25-03 | AFM - Limitations - Power Levers | 100 | 1900 | 1900C | 1900D | 200 | 2000 | 200C | 200CT | 200T | 300 | 65-A90 | 65-A90-1 | 65-A90-3 | 65-A90-4 | 99 | 99A | A100 | A100A | A100C | A200 (C-12A) | A200 (C-12C) | A200CT (C-12D) | A200CT (C-12F) | A200CT (FWC-12D) | A200CT (RC-12D) | A200CT (RC-12G) | A200CT (RC-12H) | A200CT (RC-12K) | A200CT (RC-12P) | A200CT (RC-12Q) | A99 | A99A | B100 | B200 | B200C | B200CT | B200T | B300 | B300C (C-12W) | B90 | B99 | C90 | C90A | C99 | E90 | F90 | H90 |